Device and system for decomposing and oxidizing gaseous pollutant

ABSTRACT

The invention provides a device and system for decomposing and oxidizing of gaseous pollutants. A novel reaction portion reduces particle formation in fluids during treatment, thereby improving the defect of particle accumulation in a reaction portion. Also, the system includes the device, wherein a modular design enables the system to have the advantage of easy repair and maintenance.

CROSS-REFERENCE TO RELATED APPLICATION

This application is a continuation application, filed under 35 U.S.C. §371, of International Patent Application No. PCT/SG2018/050332, filed onJul. 5, 2018, which claims priority to U.S. Provisional Application No.62/529,795, filed on Jul. 7, 2017, the entire contents of which areincorporated herein by reference.

FIELD OF THE INVENTION

The present invention relates to a device for gaseous pollutants, andmore particularly to a device for controlling the decompositionoxidation of a gaseous pollutant in semiconductor or other industrialmanufacturing processes.

BACKGROUND OF THE INVENTION

Various chemicals used in the semiconductor manufacturing process, aswell as toxic by-products that may be produced, will cause significantharm to human bodies and the environment. Examples of these chemicalsinclude mixed gases containing antimony, arsenic, boron, germanium,nitrogen, phosphorus, silicon, selenium, halogen, halogen silane, orperfluoro compounds (PFCs), or by-products formed by the decompositionof the perfluoro compounds (PFCs).

In the conventional art, the harmful mixed gases or by-products areprocessed through a device for decomposing and oxidizing a gaseouspollutant, converted into products with lower environmental harm, andthen discharged into the environment.

However, there are imperfections in the conventional device fordecomposing and oxidizing of a gaseous pollutant. For example, in thecurrently used device, particles such as silicon oxide are easily formedand deposited on a wall of a combustion chamber of the device, resultingin blocking of the combustion chamber and problems such as incompletecombustion. In order to avoid the above problems and prolong the servicelife of the device, it is bound to clean the device more frequently andinput more cost for maintaining the device. However, the maintenanceprocedure for the device is a disadvantage in labor resources and costfor manufacturers.

In order to improve the above disadvantage and other deficiencies, manyresearch teams have made active development. For example, in U.S. Pat.No. 7,985,379B2 discloses a thermal reaction chamber designed with astructure of stacked mesh ceramic rings in order to reduce theaccumulation of particles generated during the reaction When air passesthrough holes of the mesh ceramic rings, a boundary like structure isformed to prevented the particles from being deposited on an inner wallof the thermal reaction chamber. The patent also proposes other methodsto avoid particle deposition. For example, an inner wall of a gas inletpassage is electrically polished to make the mechanical roughness (Ra)lower than 30, making it difficult for particles to adhere to a wastegas. The above method can only reduce particle attachment as much aspossible, but the effect is limited. From another perspective, how toreduce the generation of particles may also be a direction that can befocused on, and further research is urgently needed.

SUMMARY OF THE INVENTION

A main object of the invention is to solve the problem that in aconventional emission reduction system, a combustion chamber is prone toincomplete combustion due to blockage.

In order to achieve the above object, the invention provides a devicefor controlling the decomposition and oxidation of a gaseous pollutant.The device not only can reduce the problem of particle residue in thedevice, but also has the advantage of being easy to clean and maintain.

Specifically, an embodiment of the invention provides a device fordecomposing and oxidizing a gaseous pollutant. The device includes areaction portion, a washing portion, a hydraulic cyclone portion, and awater tank connected to the reaction portion, the washing portion andthe hydraulic cyclone portion. The device is characterized in that thereaction portion includes a first cavity including a first inner wallwhich is annular and a first outer wall arranged concentrically with thefirst inner wall, the first inner wall defining a first chamber, thefirst outer wall provided with at least one waste gas inlet passage thatpenetrates the first outer wall and the first inner wall to communicatewith the first chamber, the waste gas inlet passage including a firstmember, a second member and a connecting member, wherein both ends ofthe connecting member are connected to the first member and the secondmember respectively, the first member extends in a horizontal direction,one end not connected to the connecting member communicates with thefirst chamber, and the second member extends in a vertical direction; afirst intermediate section, including a first inner ring wall, a firstouter ring wall arranged concentrically with the first inner ring wall,at least one gas passage arranged between the first inner ring wall andthe first outer ring wall and communicating with the first chamber tosupply a fuel, and a pilot flame inlet provided in the first inner ringwall, the first inner ring wall defining a first internal spacecommunicating with the first cavity; a second cavity, including a secondinner wall which is annular and a second outer wall arrangedconcentrically with the second inner wall, the second inner walldefining a second chamber communicating with the first intermediatesection, the second outer wall including at least one gas inlet passagefor a gas to flow inward to the second chamber; a second intermediatesection, including a second inner ring wall and a second outer ring wallarranged concentrically with the second inner ring wall, the secondinner ring wall defining a second internal space communicating with thesecond cavity; and a third cavity including a second inner wall which isannular and a third outer wall arranged concentrically with the thirdinner wall, the third inner wall defining a third chamber communicatingwith the second intermediate section, at least one liquid passagearranged on the third outer wall and penetrating the third inner wall tointroduce a liquid into the third chamber.

One embodiment of the invention provides a device for decomposing andoxidizing a gaseous pollutant. The device includes a reaction portion, awashing portion, a hydraulic cyclone portion, and a water tank connectedto the reaction portion, the washing portion and the hydraulic cycloneportion. The device is characterized in that the reaction portionincludes a first cavity including a first inner wall which is annularand a first outer wall arranged concentrically with the first innerwall, the first inner wall defining a first chamber, the first outerwall provided with at least one waste gas inlet passage that penetratesthe first outer wall and the first inner wall to communicate with thefirst chamber; a first intermediate section, including a first innerring wall, a first outer ring wall arranged concentrically with thefirst inner ring wall, at least one gas passage arranged between thefirst inner ring wall and the first outer ring wall and communicatingwith the first chamber to supply a fuel, and a pilot flame inletprovided in the first inner ring wall, wherein the first inner ring walldefines a first internal space communicating with the first cavity; asecond cavity, including a second inner wall which is annular and asecond outer wall arranged concentrically with the second inner wall,the second inner wall defining a second chamber communicating with thefirst intermediate section, a second intermediate section including asecond inner ring wall and a second outer ring wall arrangedconcentrically with the second inner ring wall, the second inner ringwall defining a second internal space communicating with the secondcavity; and a third cavity including a third inner wall which is annularand a third outer wall arranged concentrically with the third innerwall, the third inner wall defining a third chamber communicating withthe second intermediate section, at least one liquid passage arranged onthe third outer wall and penetrating the third inner wall to introduce aliquid into the third chamber.

The invention provides a system for decomposing and oxidizing a gaseouspollutant. The system includes an equipment portion and a controlportion, and is characterized in that the equipment portion includes areaction portion, a washing portion, a hydraulic cyclone portion, and awater tank. The reaction portion, the washing portion and the hydrauliccyclone portion communicate with the water tank via at least threecommunication ports of the water tank, respectively. The control portionextends vertically upward and is arranged adjacent to one side of thereaction portion, the washing portion or the hydraulic cyclone portionin parallel. The control portion includes a plurality of controlswitches that are electrically connected to the reaction portion, thewashing portion, the hydraulic cyclone portion, and the water tank ofthe equipment portion.

The invention also provides a thermal reactor for removing a pollutantfrom a waste gas, which includes a thermal reaction unit including achamber comprising a side wall, at least one waste gas inlet penetratingthe side wall and communicating with the chamber to introduce a wastegas into the chamber in a non-longitudinal direction, a flame regionformed in the chamber and below the waste gas inlet, the waste gasenters the flame region after being introduced into the chamber andmoving downwardly by a vertical distance, and a chilling unit arrangedbelow the thermal reaction unit, connected to the thermal reaction unitand configured to receive a gas stream from the thermal reaction unit,wherein the chilling unit includes a water curtain flowing through aninner wall of the chilling unit.

The invention also provides a thermal reactor for removing a pollutantfrom a waste gas, which includes a thermal reaction unit, including achamber, at least one waste gas inlet communicating with the chamber tointroduce a waste gas into the chamber, at least one fuel inletcommunicating with the chamber to introduce a fuel which is used in adecomposition process of the waste gas in the chamber, and a pilot flameinlet communicating with the chamber to ignite the fuel, wherein thefuel inlet and the pilot flame inlet are provided below the waste gasinlet, and the waste gas inlet is spaced apart from the fuel inlet andthe pilot flame inlet by a delayed combustion distance, and a chillingunit arranged below the thermal reaction unit, connected to the thermalreaction unit and configured to receive a gas stream from the thermalreaction unit, wherein the chilling unit includes a water curtainflowing through flowing through an inner wall of the chilling unit.

The invention also provides a thermal reactor for removing a pollutantfrom a waste gas, which includes a thermal reaction unit including achamber and at least one waste gas inlet, the waste gas inletcommunicating with the chamber to introduce a waste gas into thechamber, an ignition unit arranged below the thermal reaction unit andconnected to the thermal reaction unit, the ignition unit including aflame chamber communicating with the chamber, the flame chamberincluding a fuel and a pilot flame for igniting the fuel, wherein thewaste gas enters the chamber and moving downwardly along a verticaldistance and then enters the flame chamber, and a chilling unit arrangedbelow the thermal reaction unit, connected to the thermal reaction unitand configured to receive a gas stream from the thermal reaction unit,wherein the chilling unit includes a water curtain flowing through aninner wall of the chilling unit.

The invention provides a thermal reactor for removing a pollutant from awaste gas, which includes a thermal reaction unit including a chamberand at least one waste gas inlet, the waste gas inlet communicating withthe chamber to introduce a waste gas into the chamber, an ignition unitconnected to the thermal reaction unit, the ignition unit including aflame chamber communicating with the chamber, the flame chamberincluding a fuel and a pilot flame for igniting the fuel, wherein agradually increasing temperature gradient is formed between the wastegas inlet and the pilot flame along a vertical axis, and a chilling unitarranged below the thermal reaction unit, connected to the thermalreaction unit and configured to receive a gas stream from the thermalreaction unit, wherein the chilling unit includes a water curtainflowing through an inner wall of the chilling unit.

The invention provides a thermal reactor for removing a pollutant from awaste gas, which includes a thermal reaction unit including a chamberand at least one waste gas inlet, the waste gas inlet communicating withh the chamber to introduce a waste gas into the chamber, an ignitionunit arranged below the thermal reaction unit and connected to thethermal reaction unit, the ignition unit including an outer wall, aninner wall, a premixing chamber defined between the outer wall and theinner wall, and a flame chamber defined by the inner wall, and achilling unit arranged below the thermal reaction unit, connected to thethermal reaction unit and configured to receive a gas stream from thethermal reaction unit, wherein the chilling unit includes a watercurtain flowing through an inner wall of the chilling unit.

The invention provides a thermal reactor for removing a pollutant from awaste gas, which includes a first thermal reaction unit including achamber and at least one waste gas inlet, the waste gas inletcommunicating with the chamber to introduce a waste gas into thechamber, an ignition unit arranged below the first thermal reactionunit, the ignition unit including a flame chamber that communicates withthe chamber, the flame chamber including a fuel and a pilot flame forigniting the fuel, a second thermal reaction unit arranged below theignition unit, the second thermal reaction unit including an inclinedinner wall, a conical chamber defined by the inclined inner wall, and atleast one gas inlet passage that penetrates the inclined inner wall andprovides a gas flow, wherein the gas flow is sprayed obliquely downwardinto the conical chamber to slow down the deposition of particles of thewaste gas on the inclined inner wall, and a chilling unit arranged belowthe second thermal reaction unit, connected to the second thermalreaction unit and configured to receive a gas stream from the secondthermal reaction unit, wherein the chilling unit includes a watercurtain flowing through an inner wall of the chilling unit.

Therefore, the effects achieved by the invention compared with theconventional device are as follows:

(1) With a two-stage reaction portion of the invention, after the wastegas entering the reaction portion, the waste gas first moves by adistance and then be gradually heated. Compared with a conventionaldevice, when the waste gas is immediately combusted after entering thedevice, the invention can effectively reduce the problem of incompletecombustion caused by particles in the waste gas blocking a combustionchamber.

(2) In the invention, a charge coupled device (CCD) sensor is providedto directly detect the temperature of the first chamber. Compared withthe conventional device, the temperature of the first chamber can alsobe controlled directly and effectively.

The system for controlling the decomposition and oxidation of a gaseouspollutant of the invention comprises a plurality of openings on ahousing, which are arranged correspondingly to the devices accommodatedtherein in a modular manner, so it has the advantage of easymaintenance.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1A is a front view of a device for decomposing and oxidizing of agaseous pollutant according to an embodiment of the invention.

FIG. 1B is a rear view of a device for decomposing and oxidizing of agaseous pollutant according to an embodiment of the invention.

FIG. 2 is a cross-sectional schematic view of a first cavity accordingto an embodiment of the invention.

FIG. 3 is a schematic view of a first cavity according to an embodimentof the invention.

FIG. 4A is a schematic view of a first intermediate section according toan embodiment of the invention.

FIG. 4B is a partial cross-sectional schematic view of FIG. 4A.

FIG. 5 is a cross-sectional schematic view of a second cavity accordingto an embodiment of the invention.

FIG. 6 is a cross-sectional schematic view of a second intermediatesection according to an embodiment of the invention.

FIG. 7 is a cross-sectional schematic view of a third cavity accordingto an embodiment of the invention.

FIG. 8 is a schematic view of a washing portion according to anembodiment of the invention.

FIG. 9 is a schematic view of a water tank according to an embodiment ofthe invention.

FIG. 10 is a schematic view of a system for decomposing and oxidizing ofa gaseous pollutant according to an embodiment of the invention.

FIG. 11 is a schematic view of a system for decomposing and oxidizing ofa gaseous pollutant according to another embodiment of the invention.

FIG. 12 is a schematic view of a thermal reactor for removing apollutant from waste gas according to an embodiment of the invention.

FIG. 13 is a schematic view of another embodiment of a waste gas inletin FIG. 12.

FIG. 14 is a schematic view of a thermal reactor for removing apollutant from waste gas according to another embodiment of theinvention.

FIG. 15 is a schematic view of a temperature gradient of A-A′ in FIG.14.

FIG. 16 is a schematic view of a thermal reactor for removing apollutant from waste gas according to another embodiment of theinvention.

FIG. 17 is a schematic view of a thermal reactor for removing apollutant from waste gas according to other embodiments of theinvention.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

The detailed description and technical contents of the disclosure areexplained below with reference to the drawings.

FIG. 1A and FIG. 1B are a front view and a rear view of a device 1 fordecomposing and oxidizing a gaseous pollutant according to an embodimentof the disclosure, respectively. The device 1 includes a reactionportion 10, a washing portion 20, a hydraulic cyclone portion 30, and awater tank 40 connected to the reaction portion 10, the washing portion20 and the hydraulic cyclone portion 30, respectively.

The reaction portion 10 has a top and a bottom, and sequentiallyincludes a first cavity 11, a first intermediate section 12, a secondcavity 13, a second intermediate section 14, and a third cavity 15, fromthe top to the bottom.

Refer to FIG. 2, the first cavity 11 includes a first inner wall 111 anda first outer wall 112. The first inner wall 111 is annular to define afirst chamber 113. The first outer wall 112 surrounds the first innerwall 111 and is arranged concentrically with the first inner wall 111.At least one waste gas inlet passage 114 is provided on the first outerwall 112. The waste gas inlet passage 114 penetrates the first outerwall 112 and the first inner wall 111 and communicates with the firstchamber 113 to let waste gas (or exhaust gas) enter the first chamber113 via the waste gas inlet passage 114. In one embodiment, the wastegas is an effluent stream from one or more process chambers.Non-limiting examples of such process chambers include substrateprocessing systems used in, for example, semiconductor, flat panel,photovoltaic or other silicon and thin film processing applications.

Refer to FIG. 2 and FIG. 3, in one embodiment, the waste gas inletpassage 114 includes a first member 1141, a second member 1142 and aconnecting member 1143. Both ends of the connecting member 1143 areconnected to the first member 1141 and the second member 1142,respectively. Taking a ground as a reference, the first member 1141extends in a horizontal direction with the ground, and one end notconnected to the connecting member 1143 connects with the first chamber113. The second member 1142 extends in a perpendicular direction withthe ground and the second member 1142 is parallel to the direction inwhich the first cavity 11 is arranged. An angle between the first member1141 and the first outer wall 112 is between 75° and 135°. In apreferred embodiment, the angle is ranged from 75° to 90°, and morespecifically in 90°. Therefore, compared with a conventional waste gasinlet passage that is only a long pipe vertically inserted into achamber, the device 1 for decomposing and oxidizing a gaseous pollutantprolongs the moving time of waste gas in the device 1, therebypreventing the waste gas from entering the first chamber 113 too quicklyto be combusted. In the present invention, the diameter of the waste gasinlet passage 114 is not particularly limited and could be changed asrequired.

Compared with the conventional device, the size of the reaction portion10 and the waste gas inlet passage 114 in the invention is much smaller.In one embodiment, the height from a top of the first chamber 113 to abottom of the water tank 40 is less than 160 cm, and preferably lessthan 150 cm. In the invention, it may be changed as required.

Refer to FIG. 3, H1 is defined as a distance between a position of thewaste gas inlet passage 114 on the first outer wall 112 and the top ofthe first outer wall 112, and H2 is defined as a distance between theposition of the waste gas inlet passage 114 on the first outer wall 112and the bottom of the first outer wall 112. In one embodiment, H1 isgreater than H2; and in another embodiments, H1 may be equal to orsmaller than H2 as required. Accordingly, neither H1 nor H2 is 0, andspecifically H2 is between 4 inches and 5 inches. Compared with atechnology that waste gas is combusted as soon as it enters a chamber ofa conventional device, waste gas of the invention needs to move adistance of H2 before be combusted in the first intermediate section 12when waste gas is introduced into the first chamber 113. Therefore,waste gas would be heated beforehand, which effectively reduces theconcentration phenomenon for generating particles caused by theexcessive temperature difference of waste gas, thereby reducing theprobability that particles are deposited or blocked in the first chamber113.

In one embodiment, the reaction portion 10 further includes an uppercover plate 16. The upper cover plate 16 is arranged on the top of thefirst cavity 11. In another embodiment, the upper cover plate 16 is onlyplaced on the top of the first chamber 113 without containing anyconnection components, thereby blocking the communication between thefirst chamber 113 and the outside. Also, in other embodiments, the uppercover plate 16 is connected to the first cavity 11 via a pivot member tobe opened or closed by flip. In one embodiment, the waste gas inletpassage 114 is deliberately not arranged on the upper cover plate 16,but is arranged on a side wall of the first cavity 11, so as to createthe effect of delayed combustion of the waste gas to achieve asufficient reaction. In other embodiment, the waste gas inlet passage114 is arranged on the upper cover plate 16, and through the combinationof other structures, the effect of delayed combustion of the waste gasis also achieved.

Refer to FIG. 4A and FIG. 4B, the first intermediate section 12 isconnected to the bottom of the first cavity 11 and is a position wherethe combustion starts. The first intermediate section 12 includes afirst inner ring wall 121, a first outer ring wall 122 arrangedconcentrically with the first inner ring wall 121, a first intermediatespace 123, a first gas passage 124, a second gas passage 125, and acooling water passage 126. In other embodiment, the first intermediatesection 12 further includes an upper gas passage 127 a and a lower gaspassage 127 b, or includes an upper gas passage 127 a and a lower gaspassage 127 b to replace the first gas passage 124 and the second gaspassage 125.

The first inner ring wall 121 defines a first internal space 1211, whichcommunicates with the first chamber 113. The first intermediate space123 is defined between the first inner ring wall 121 and the first outerring wall 122. The first inner ring wall 121 includes a plurality ofnozzles 1212 and at least one pilot flame inlet 1213. The first gaspassage 124 and the second gas passage 125 respectively pass through thefirst outer ring wall 122 and communicate with the first intermediatespace 123. In one embodiment, the cooling water passage 126 is arrangedoutside of the first outer ring wall 122. Thus, the purpose ofcontrolling the temperature of the first intermediate space 123 isachieved by flowing the cooling water through the cooling water passage126. The upper gas passage 127 a and the lower gas passage 127 b arerespectively arranged on an upper surface and a lower surface of thefirst intermediate section 12, and the upper gas passage 127 a, thelower gas passage 127 b and the first intermediate space 123 communicatewith each other via through holes (not shown in figures), respectively.

In the first intermediate section 12, at least two kinds of gases aremixed into a fuel-rich gas, which is introduced into the first internalspace 1211 to match with a pilot flame provided by the pilot flame inlet1213 to generate combustion at a high temperature in the first internalspace 1211. For example, the high temperature of the first internalspace 1211 is more than 500° C., such as ranged between 500° C. and2500° C. Regarding the gas delivery configuration of the firstintermediate section 12, there are the following types:

In one embodiment, a first gas enters the first intermediate space 123through the first gas passage 124, a second gas enters the firstintermediate space 123 through the second gas passage 125. The first gasand the second gas are mixed in the first intermediate space 123 andthen conveyed into the first internal space 1211 through the pluralityof nozzles 1212. In another embodiment, the first gas and the second gasare first mixed outside into a premixed gas. Then, the premixed gasenters the first intermediate space 123 through the first gas passage124 and the second gas passage 125 respectively, which are further mixedin the first intermediate space 123, and then conveyed into the firstinternal space 1211 through the plurality of nozzles 1212. In anotherembodiment, the first gas passes through the upper gas passage 127 a andenters the first intermediate space 123 downwardly. The second gaspasses through the lower gas passage 127 b and enters the firstintermediate space 123 upwardly. The first gas and the second gas aremixed in the first intermediate space 123, and then conveyed into thefirst internal space 1211 through the plurality of nozzles 1212. Inanother embodiment, the first gas and the second gas are first mixedoutside into a premixed gas. Then, the premixed gas enters the firstintermediate space 123 through the upper gas passage 127 a and the lowergas passage 127 b respectively, which are further mixed in the firstintermediate space 123, and then conveyed into the first internal space1211 through the plurality of nozzles 1212. The first gas may be a fuel,including but not limited to hydrogen, methane, natural gas, propane,liquefied petroleum gas (LPG), or a mixture of the foregoing. The secondgas may be an oxidant, including but not limited to oxygen, ozone, air,compressed dry air (CDA), oxygen-rich air, or a mixture of theforegoing.

The gas pipeline configuration in the first intermediate section 12could be adjusted as required, to introduce a combustion-assisting gasinto the first intermediate space 123 in a ring shape, and then into thefirst internal space 1211 below the first cavity 11 to generate ahigh-temperature combustion environment, whereby the gas pipelineconfiguration is not limited to the above-mentioned configuration.

The pilot flame is formed by igniting the first intermediate section 12or is formed in a specially designed pilot body, and then guided intothe first intermediate section 12, to reduce the flameout problem in agas inlet passage caused by gas increased suddenly (not shown infigures). The first intermediate space 123 further includes an annularpassage 1231 to allow cooling water to flow through, thereby achievingthe purpose of controlling the temperature of the first intermediatespace 123.

Refer to FIG. 1A, FIG. 3 and FIG. 4A together, the plurality of nozzles1212 and the pilot flame inlet 1213 are provided below the waste gasinlet passage 114 and designed to be spaced apart by a distance. In thisway, after waste gas enters the first chamber 113, it will movedownwardly along the vertical distance H2 to pass through a temperaturegradient region, and then enter a flame environment of the firstintermediate section 12. Thus, it avoids the problem of incompletedecomposition or particle deposition caused by waste gas directlyentering the high-temperature flame environment too quickly.

Refer to FIG. 1A and FIG. 5, the second cavity 13 is in an oxygen-richreaction state to oxidize carbon monoxide to form carbon dioxide. Thesecond cavity 13 includes a second inner wall 131 and a second outerwall 132 arranged concentrically with the second inner wall 131. Thesecond inner wall 131 defines a second chamber 133, which iscommunicated with the first internal space 1211 and the first chamber113. The second chamber 133 is a tank for gas flowing inwardly, whichcan avoid particle deposition and reduce the probability of particlesblocking the second inner wall 131. For the purpose of continuouscombustion, a gas inlet passage 1321 is arranged on the second outerwall 132, which passes through the second inner wall 131 to introduce agas into the second chamber 133. In one embodiment, the gas is oxygen.

Refer to FIG. 6, the second intermediate section 14 includes a secondinner ring wall 141 and a second outer ring wall 142 arrangedconcentrically with the second inner ring wall 141. At least one oxidantpassage 1421 is arranged on the second outer ring wall 142 forintroducing an oxidant. A second internal space 1411 is defined thesecond inner ring wall 141, and a second intermediate space 143 isdefined between the second inner ring wall 141 and the second outer ringwall 142. The second internal space 1411 communicates with the secondchamber 133. The oxidant passage 1421 passes through the second innerring wall 141 to introduce the oxidant into the second internal space1411 via the second intermediate space 143. In one preferred embodiment,the amount of introduced oxidants is sufficient to convert a fuel-richstate fluid from the second chamber 133 to a fuel-lean mixture.

Refer to FIG. 6 and FIG. 7, the third cavity 15 is a cooling cavity,which is cooled by spraying a liquid to a fluid flowing therethrough. Inone preferred embodiment, the liquid is a water flow. The third cavity15 includes a third inner wall 151 and a third outer wall 152 arrangedconcentrically with the third inner wall 151. The third inner wall 151defines a third chamber 153, and the third chamber 153 communicates withthe second internal space 1411 and the second chamber 133. At least oneliquid passage 154 is arranged on the third outer wall 152 andpenetrates the third outer wall 152. A storage space 155 is providedbetween the third inner wall 151 and the third outer wall 152.Therefore, when the water is introduced from the liquid passage 154, thestorage space 155 will be gradually filled, and finally the wateroverflows from the storage space 155 to form a waterfall flow, whichflows down along the third inner wall 151, thereby reducing thedeposition and aggregation of particles in the reaction portion 10.

The reaction portion 10 of the device 1 for decomposing and oxidizing agaseous pollutant belongs to a two-stage combustion reaction portion.The formation of NO_(x) and CO is minimized through the step-by-stepdesign of the first chamber 113 and the second chamber 133. According tothe experimental results, the NO_(x) of the device 1 for decomposing andoxidizing a gaseous pollutant is below the detection limit of 15 ppm NOand 20 ppm NO₂.

Refer to FIG. 8, the washing portion 20 is a long cylindrical shape andincludes a plurality of fillers (not shown in figures) to increase acontact area between the waste gas and the fillers. In addition, aninner wall of the washing portion 20 is provided with a plurality ofjets (not shown in figures), and at positions of the washing portion 20higher than the plurality of fillers are provided with a plurality ofdrippers 23. For example, the plurality of fillers is made of polyvinylchloride (PVC), but is not limited to the above materials. The pluralityof jets provides an effluent treating agent between the plurality offillers to remove residues remaining between the plurality of fillers asa fluid flowing through. As for the plurality of drippers 23, theeffluent treating agent is provided in the form of large drops to wetand rinse the plurality of fillers from above. In an embodiment, theparticle capture rate is increased by increasing the wet area of thewashing portion 20 while reducing the flow rate of the fluid.

FIG. 9 is a schematic view of the water tank 40 according to oneembodiment thereof. The water tank 40 includes a front surface 41, arear surface 42 opposite to the front surface 41, and a top surface 43connecting the front surface 41 and the rear surface 42. The top surface43 includes at least three communication ports 431, which respectivelycommunicate with the reaction portion 10, the washing portion 20, andthe hydraulic cyclone portion 30 (not shown in FIG. 9). In addition, thefront surface 41 and/or the rear surface 42 are provided with at leastone opening portion 44. As to the opening portion 44, the water tank 40is easily cleaned without removing other components such as the reactionportion 10 or the washing portion 20.

Besides, in one embodiment, a water spray unit (not shown in figures) isarranged at a position where the fluid flows out of the third cavity 15of the reaction portion 10, thereby preventing particles in the fluidfrom entering the washing portion 20. In another embodiment, a pH sensor(not shown in figures) is arranged on the top surface 43 of the watertank 40 to monitor the pH concentration in the water tank 40, and areal-time alarm is given when the value is abnormal. Or, in otherembodiments, a water amount monitor (not shown in figures) is used tomonitor the amount of water in the water tank 40 to avoid exceeding amaximum allowable range.

The hydraulic cyclone portion 30 is connected to the water tank 40 as afilter to capture the particles in the water tank 40, thereby prolongingthe maintenance period of the device 1. Please refer to FIG. 1B. In theinvention, a sensor 50 is further included, and the type of the sensor50 may be selected as required. For example, respecting the reactionportion 10 is monitored through the sensor 50 to obtain a betterperformance of destruction and removal efficiency (DRE), a temperaturesensor capable of detecting the temperature during combustion in timecould be used, such as a resistance temperature detector (RTD), athermocouple, a thermistor, an infrared sensor, a semiconductor sensor,and a thermometer, but are not limited to above. The sensor 50penetrates into any one or more chambers in the reaction portion 10, anddetects or monitors the status of waste gas reaction in real time.

In one embodiment, the sensor 50 is a charge coupled device (CCD) usedto monitor the combustion temperature. The charge coupled device (CCD)is installed on the upper cover plate 16, wherein an end of the chargecoupled device (CCD) passes through the upper cover plate 16 and entersthe first chamber 113 (please refer to FIG. 1A, FIG. 1B and FIG. 2together). Or, the charge coupled device (CCD) is arranged on the firstouter wall 112 of the first cavity 11, wherein an end of the chargecoupled device (CCD) passes through the first outer wall 112 and entersthe first chamber 113 for monitoring (not shown in figures). Pleaserefer to FIG. 10, the device 1 of the invention further includes ahuman-machine interface to allow a user to remotely monitor and remotelycontrol the device 1 via an appropriate wired or wireless device 80(such as a smart phone). The connection between the charge coupleddevice (CCD) and the human-machine interface may be wired or wireless,and is not limited thereto.

The invention further integrates the above-mentioned device 1 with acontrol portion 70 into a system for controlling the decomposing andoxidizing a gaseous pollutant.

Please refer to FIG. 10. The system includes an equipment portion (i.e.,the device 1) and the control portion 70. The components of theequipment portion are as described above, and will not be describedhere. The control portion 70 extends vertically upward and is arrangedadjacent to one side of the device 1 in parallel. The control portion 70includes a plurality of control switches that are electrically andrespectively connected to the reaction portion 10, the washing portion20, the hydraulic cyclone portion 30 (not shown in FIG. 10), and thewater tank 40 of the device 1 in order to control the device 1.

The invention may further utilize the aforementioned wired or wirelessdevice 80 to remotely control the control portion 70, as shown in FIG.10.

In one embodiment, the device 1 is installed in a housing 2 as shown inFIG. 11, and further includes a pump 60.

In one embodiment, an opening on the back side of a housing of thedevice 1 is removed, and then another casing that accommodates the pump60 is combined with the device 1. Accordingly, the regions of othermanufacturing devices (such as the pump 60) are reduced, so that moretools are allowed to be installed in a limited space, and theinterconnection wiring of the pump 60 is reduced, thereby achieving thepurpose of reducing installation costs and saving time.

The invention also provides a thermal reactor 90 for removing apollutant from a waste gas. Please refer to FIG. 12. In one embodiment,the thermal reactor 90 includes a thermal reaction unit 91 and achilling unit 92. The thermal reaction unit 91 includes a chamber 911,at least one waste gas inlet 912 and a flame region 913. The chamber 911comprises a side wall 914, and the waste gas inlet 912 penetrates theside wall 914 and communicates with the chamber 911 to introduce a wastegas G_(w) into the chamber 911 in a non-longitudinal direction. Theflame region 913 is formed in the chamber 911 and is located below thewaste gas inlet 912, so that after the waste gas G_(w) is introducedinto the chamber 911, it moves downwardly along a vertical distanceD_(v) to enters the flame region 913. In the embodiment, thenon-longitudinal direction is a horizontal direction. In otherembodiments, the non-longitudinal direction may be other non-verticaland oblique direction that comprises an angle less than 90 degrees witha horizontal plane, as shown in FIG. 13. In this way, when the waste gasG_(w) is introduced into the chamber 911, it will not immediatelycontact the flame region 913. Therefore, the thermal reactor 90 has aneffect of preventing the waste gas G_(w) from being deposited on aninner wall of the chamber 911 due to incomplete decomposition. Thechilling unit 92 is arranged below and connected to the thermal reactionunit 91, and the chilling unit 92 is configured to receive a gas streamGs from the thermal reaction unit 91. The chilling unit 92 includes awater curtain W flowing through an inner wall 921 of the chilling unit92.

In the embodiment, the thermal reaction unit 91 further includes atleast one fuel inlet 915 and a pilot flame inlet 916. The fuel inlet 915introduces a fuel F into the chamber 911. The pilot flame inlet 916provides a pilot flame 917 for igniting the fuel F. In FIG. 12 and FIG.13, the fuel inlet 915 and the pilot flame inlet 916 are provided belowthe waste gas inlet 912, but are not limited to. In other examples, thefuel inlet 915 and the pilot flame inlet 916 may be optionally providedat other positions, as long as the flame region 913 is formed in thechamber 911 and is located below the waste gas inlet 912. In addition,in an embodiment, the fuel F may be mixed with an air or another gas ina premixing chamber 918 and then conveyed to the chamber 911.

In another embodiment, please also refer to FIG. 12 and FIG. 13. Thethermal reactor 90 includes a thermal reaction unit 91 and a chillingunit 92. The thermal reaction unit 91 includes a chamber 911, at leastone waste gas inlet 912, at least one fuel inlet 915, and a pilot flameinlet 916. The waste gas inlet 912 communicates with the chamber 911 tointroduce a waste gas G_(w) into the chamber 911. The fuel inlet 915communicates with the chamber 911 to introduce a fuel F. The fuel F isused in a decomposition process of the waste gas G_(w) in the chamber911. The pilot flame inlet 916 communicates with the chamber 911 toprovide a pilot flame 917 for igniting the fuel F. In the embodiment,the fuel inlet 915 and the pilot flame inlet 916 are provided below thewaste gas inlet 912, and are separated apart from the waste gas inlet912 by a delayed combustion distance D_(d). The chilling unit 92 isarranged below and connected to the thermal reaction unit 91, and thechilling unit 92 is configured to receive a gas stream G_(s) from thethermal reaction unit 91. The chilling unit 92 includes a water curtainW flowing through an inner wall 921 of the chilling unit 92. In FIG. 12and FIG. 13, the waste gas inlet 912 penetrates the side wall 914 andcommunicates with the chamber 911 to introduce a waste gas G_(w) intothe chamber 911 in a non-longitudinal direction. However, in otherembodiments, the waste gas inlet 912 may introduce the waste gas G_(w)into the chamber 911 in other directions, as long as the fuel inlet 915and the pilot flame inlet 916 are provided below the waste gas inlet 912and spaced apart by the delayed combustion distance D_(d), for thepurpose of delayed ignition.

In another embodiment, please refer to FIG. 14. The thermal reactor 90includes a thermal reaction unit 91, a chilling unit 92 and an ignitionunit 93. The thermal reaction unit 91 includes a chamber 911 and atleast one waste gas inlet 912. The waste gas inlet 912 communicates withthe chamber 911 to introduce a waste gas G_(w) into the chamber 911. Theignition unit 93 is connected to the thermal reaction unit 91. Theignition unit 93 includes a flame chamber 931. The flame chamber 931communicates with the chamber 911. The flame chamber 931 includes a fuelF, a pilot flame 932 for igniting the fuel F, at least one fuel inlet933, and a pilot flame inlet 934. The fuel inlet 933 introduces the fuelF into the chamber 911, and the pilot flame inlet 934 provides the pilotflame 932. The chilling unit 92 is arranged below and connected to thethermal reaction unit 91, and the chilling unit 92 is configured toreceive a gas stream G_(s) from the thermal reaction unit 91. Thechilling unit 92 includes a water curtain W flowing through an innerwall 921 of the chilling unit 92. In the embodiment, the waste gas G_(w)enters the flame chamber 931 after entering the chamber 911 downward fora vertical distance D_(v).

In another embodiment, a temperature gradient which gradually increasestemperature downward is formed between the waste gas inlet 912 and thepilot flame 932 along a vertical axis. That is, from a part A adjacentto the waste gas inlet 912 to a part A′ of the flame chamber 931, thetemperature gradient gradually increases, as shown in FIG. 15. In theembodiment, the angle of the waste gas inlet 912, the arrangementpositions of the fuel inlet 915 and the pilot flame inlet 916, or thearrangement position of the flame region 913 may refer to theabove-mentioned FIG. 12, FIG. 13, and FIG. 14. Or, other designs mayalso be adopted, as long as the temperature gradient is formed betweenthe waste gas inlet 912 and the pilot flame 932.

In other embodiments, please refer to FIG. 12 or FIG. 13. The thermalreactor 90 includes a thermal reaction unit 91 and a chilling unit 92.The thermal reaction unit 91 includes a chamber 911 and at least onewaste gas inlet 912. The waste gas inlet 912 communicates with thechamber 911 to introduce a waste gas G_(w) into the chamber 911. Thechilling unit 92 is arranged below and connected to the thermal reactionunit 91, and the chilling unit 92 is configured to receive a gas streamG_(s) from the thermal reaction unit 91. The chilling unit 92 includes awater curtain W flowing through an inner wall 921 of the chilling unit92.

In another embodiment, please refer to FIG. 14. The thermal reactor 90includes a thermal reaction unit 91, a chilling unit 92 and an ignitionunit 93. The thermal reaction unit 91 includes a chamber 911 and atleast one waste gas inlet 912. The waste gas inlet 912 communicates withthe chamber 911 to introduce a waste gas G_(w) into the chamber 911. Theignition unit 93 is arranged below the thermal reaction unit 91 andconnected to the thermal reaction unit 91. The ignition unit 93 includesan outer wall, an inner wall, a premixing chamber defined between theouter wall and the inner wall, and a flame chamber 931 defined by theinner wall. FIG. 4A and FIG. 4B show the structure of the ignition unit93. The chilling unit 92 is arranged below and connected to the ignitionunit 93, and the chilling unit 92 is configured to receive a gas streamG_(s) from the thermal reaction unit 91. The chilling unit 92 includes awater curtain W flowing through an inner wall 921 of the chilling unit92.

In another embodiment, please refer to FIG. 16. The thermal reactor 90includes a first thermal reaction unit 91A, a chilling unit 92, anignition unit 93, a second thermal reaction unit 94, and an oxygen-richgas supply unit 95. The first thermal reaction unit 91A includes achamber 911 and at least one waste gas inlet 912. The waste gas inlet912 communicates with the chamber 911 to introduce a waste gas G_(w)into the chamber 911. The ignition unit 93 includes a flame chamber 931.The flame chamber 931 communicates with the chamber 911. The flamechamber 931 includes a fuel F and a pilot flame 932 for igniting thefuel F. The second thermal reaction unit 94 is arranged below theignition unit 93. The second thermal reaction unit 94 includes a ceramicportion 941, an inner wall 942, a chamber 943 defined by the inner wall942, at least one gas inlet hole 944 that penetrates the inner wall 942and provides a gas flow A, and a gas flow passage 945 that supplies thegas flow A. In the embodiment, the gas flow A is a room-temperature air.The oxygen-rich gas supply unit 95 is arranged below the second thermalreaction unit 94 and includes at least one gas inlet hole 951. Theoxygen-rich gas supply unit 95 conveys an oxygen-rich gas G_(o) from thegas inlet hole 951 to the chamber 911 of the thermal reactor 90. Thechilling unit 92 is arranged below the first thermal reaction unit 91Aand communicates with the chamber 911 to receive a gas stream Gs fromthe first thermal reaction unit 91A. The chilling unit 92 includes awater curtain W flowing through an inner wall 921 of the chilling unit92.

Please refer to FIG. 17. In other embodiments, the second thermalreaction unit 94 includes an inclined inner wall 942 a, a conicalchamber 943 a defined by the inclined inner wall 942 a, and at least oneinclined gas inlet hole 944 a that penetrates the inclined inner wall942 a and provides a gas flow A. The conical chamber 943 a comprises atop opening 9431 a communicating with the flame chamber 931 and a bottomopening 9432 a having a larger diameter than the top opening 9431 a. Thegas flow A is sprayed obliquely downward into the conical chamber 943 a.By the design of the inclined inner wall 942 a, particles of the wastegas G_(w) is slowed down and deposited on the inclined inner wall 942 a.

The components in the embodiments of FIG. 12, FIG. 13, FIG. 14, FIG. 15,FIG. 16, and FIG. 17 can be cross-referenced, and can also becross-referenced to the components in the embodiments of FIG. 1, FIG. 2,FIG. 3, FIG. 4, FIG. 5, FIG. 6, FIG. 7, FIG. 8, FIG. 9, FIG. 10, FIG.11, FIG. 12, FIG. 13, FIG. 14, FIG. 15, and FIG. 16.

What is claimed is:
 1. A system for decomposing and oxidizing a gaseouspollutant, comprising an equipment portion and a control portion,wherein the equipment portion comprises a reaction portion, a washingportion, a hydraulic cyclone portion, and a water tank, wherein thereaction portion, the washing portion and the hydraulic cyclone portioncommunicate with the water tank via a top communication port of thewater tank, and wherein the reaction portion comprises a chamber, atleast one waste gas inlet connected to one side of the chamber andcommunicated with the chamber, a plurality of nozzles and at least oneinlet for an entry of a pilot flame, and wherein the at least one wastegas inlet provides waste gas to enter the chamber in a level direction,and the plurality of nozzles and the at least one inlet are communicatedwith the chamber and formed below the at least one waste gas inlet, andthe plurality of nozzles and the at least one inlet are spaced apartfrom the at least one waste gas inlet by a delayed combustion distance;and the control portion extends vertically upward and is arrangedadjacent to one side of the reaction portion, the washing portion or thehydraulic cyclone portion in parallel, the control portion comprising aplurality of control switches that are electrically connected to thereaction portion, the washing portion, the hydraulic cyclone portion,and the water tank of the equipment portion.
 2. The system of claim 1,wherein the water tank comprises a front surface, a rear surfaceopposite to the front surface, a top surface connected to the frontsurface and the rear surface separately, and at least one openingportion arranged in the surface selected from the group consisting ofthe front surface, the rear surface, and a combination thereof.